TY - GEN
T1 - Impact of Multiple Detonation Waves on Heat Flux in Rotating Detonation Engines
AU - Oh, Hyejin
AU - Li, Wenhai
AU - Ladeinde, Foluso
N1 - Publisher Copyright:
© 2025, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2025
Y1 - 2025
N2 - Rotating detonation engines (RDEs) are currently receiving significant attention for their high propulsive efficiency. These devices often operate under conditions that generate multiple detonation waves. Building on the work of Ladeinde et al. [Supersonic Combustion Heat Flux in a Rotating Detonation Engine, Acta Astronautica 203 (2023) 226-245], this study investigates the influence of multiple waves on the distributions of heat flux in RDEs, which is a critical area for optimizing engine design and enhancing thermal management. Utilizing large eddy simulation, this research analyzes the effects of the interactions between detonation waves on heat flux by comparing single and multiple waves. Additionally, the study examines how variations in wave count and configuration impact the overall thermal loads of the engine. The findings are poised to inform the development of innovative heat management strategies in RDEs, particularly under diverse operational conditions that lead to multiple waves.
AB - Rotating detonation engines (RDEs) are currently receiving significant attention for their high propulsive efficiency. These devices often operate under conditions that generate multiple detonation waves. Building on the work of Ladeinde et al. [Supersonic Combustion Heat Flux in a Rotating Detonation Engine, Acta Astronautica 203 (2023) 226-245], this study investigates the influence of multiple waves on the distributions of heat flux in RDEs, which is a critical area for optimizing engine design and enhancing thermal management. Utilizing large eddy simulation, this research analyzes the effects of the interactions between detonation waves on heat flux by comparing single and multiple waves. Additionally, the study examines how variations in wave count and configuration impact the overall thermal loads of the engine. The findings are poised to inform the development of innovative heat management strategies in RDEs, particularly under diverse operational conditions that lead to multiple waves.
UR - https://www.scopus.com/pages/publications/105001300765
U2 - 10.2514/6.2025-2316
DO - 10.2514/6.2025-2316
M3 - Conference contribution
AN - SCOPUS:105001300765
SN - 9781624107238
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
BT - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
Y2 - 6 January 2025 through 10 January 2025
ER -